FR2412891B1 - - Google Patents

Info

Publication number
FR2412891B1
FR2412891B1 FR7832714A FR7832714A FR2412891B1 FR 2412891 B1 FR2412891 B1 FR 2412891B1 FR 7832714 A FR7832714 A FR 7832714A FR 7832714 A FR7832714 A FR 7832714A FR 2412891 B1 FR2412891 B1 FR 2412891B1
Authority
FR
France
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
FR7832714A
Other languages
French (fr)
Other versions
FR2412891A1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of FR2412891A1 publication Critical patent/FR2412891A1/fr
Application granted granted Critical
Publication of FR2412891B1 publication Critical patent/FR2412891B1/fr
Granted legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00—Thermometers specially adapted for specific purposes
    • G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • G01K13/028—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow for use in total air temperature [TAT] probes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00—Thermometers specially adapted for specific purposes
    • G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Investigating Or Analyzing Materials Using Thermal Means (AREA)
FR7832714A 1977-12-22 1978-11-21 Dispositif et methode pour calculer la temperature d'entree d'une turbine Granted FR2412891A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US86348377A 1977-12-22 1977-12-22

Publications (2)

Publication Number Publication Date
FR2412891A1 FR2412891A1 (fr) 1979-07-20
FR2412891B1 true FR2412891B1 (de) 1984-06-22

Family

ID=25341170

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7832714A Granted FR2412891A1 (fr) 1977-12-22 1978-11-21 Dispositif et methode pour calculer la temperature d'entree d'une turbine

Country Status (5)

Country Link
JP (1) JPS5490409A (de)
DE (1) DE2850625A1 (de)
FR (1) FR2412891A1 (de)
GB (1) GB2011091B (de)
IT (1) IT1100560B (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4748804A (en) * 1986-12-08 1988-06-07 United Technologies Corporation Inlet total temperature synthesis for gas turbine engines
GB9410760D0 (en) * 1994-05-27 1994-07-27 Rolls Royce Plc Gas turbine engine fuel control system
US5622042A (en) * 1995-02-27 1997-04-22 Compressor Controls Corporation Method for predicting and using the exhaust gas temperatures for control of two and three shaft gas turbines
JP2004132255A (ja) 2002-10-10 2004-04-30 Mitsubishi Heavy Ind Ltd 燃焼器制御装置
GB2397395B (en) 2003-01-16 2006-04-05 Rolls Royce Plc Controlling the fuel supply to a combustor of a gas turbine engine
US6931857B2 (en) 2003-05-30 2005-08-23 United Technologies Corporation Rotor inlet temperature control for turbo machine
CA2626035C (en) 2005-10-18 2014-12-02 Alstom Technology Ltd Method for protecting the hot gas parts of a gas turbine installation from overheating and for detecting flame extinction in the combustion chamber
CN100365256C (zh) * 2005-12-26 2008-01-30 王菲 脉动式燃气轮机
DE102006037560B4 (de) * 2006-02-06 2008-06-19 Siemens Ag Verfahren und Vorrichtung zum vorausschauenden Bestimmen einer Temperaturverteilung in einer Wand einer Turbinenanlage
EP2357339A1 (de) * 2010-02-12 2011-08-17 Siemens Aktiengesellschaft Verfahren zur Bestimmung einer Verbrennerausgangstemperatur und Verfahren zur Steuerung einer Gasturbine
CN113378328B (zh) * 2021-07-05 2022-04-22 中国航发湖南动力机械研究所 一种用于控制系统的燃气涡轮前温度计算方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2809492A (en) * 1952-12-23 1957-10-15 Simmonds Aerocessories Inc Apparatus for measuring and/or controlling fuel/air ratio of gas turbines without direct gravimetric fuel metering
US3377848A (en) * 1966-08-22 1968-04-16 Gen Electric Temperature indicating means for gas turbine engines
US3789665A (en) * 1972-02-22 1974-02-05 Avco Corp Inferred measurement of the turbine inlet temperature of a gas turbine engine
US4055997A (en) * 1976-09-15 1977-11-01 United Technologies Corporation Means for calculating turbine inlet temperature of a gas turbine engine

Also Published As

Publication number Publication date
IT1100560B (it) 1985-09-28
GB2011091A (en) 1979-07-04
GB2011091B (en) 1982-04-28
FR2412891A1 (fr) 1979-07-20
JPS5490409A (en) 1979-07-18
IT7829989A0 (it) 1978-11-21
DE2850625A1 (de) 1979-06-28

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Legal Events

Date Code Title Description
ST Notification of lapse